Kenneth M. Pesyna
35Patents
8h-index
42Co-inventors
75Inventor score
Filing activity: Sep 2, 1988 → Dec 6, 2024
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9677501B2 | Three stream, variable area fixed aperture nozzle with pneumatic actuation | Emerging Cross-Sectional Technologies | 24 | Active |
| US9845768B2 | Three stream, variable area, vectorable nozzle | Emerging Cross-Sectional Technologies | 23 | Active |
| US8745990B2 | Gas turbine engine with integrated electric starter/generator | Emerging Cross-Sectional Technologies | 17 | Active |
| US8245495B2 | Mechanism for a vectoring exhaust nozzle | Performing Operations; Transporting | 16 | Active |
| US9587561B2 | Heat exchanger integrated with a gas turbine engine and adaptive flow control | Emerging Cross-Sectional Technologies | 16 | Active |
| US10494116B2 | Heat shield for signature suppression system | Emerging Cross-Sectional Technologies | 9 | Active |
| US10513981B2 | Heat exchanger assembly for a gas turbine engine propulsion system | Emerging Cross-Sectional Technologies | 9 | Active |
| US4884748A | Fairing flap arrangement | Emerging Cross-Sectional Technologies | 9 | Expired |
| US10677166B2 | Heat exchanger for a gas turbine engine propulsion system | Emerging Cross-Sectional Technologies | 8 | Active |
| US9517843B2 | Generator for flight vehicle | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US7836681B2 | Mechanism for a vectoring exhaust nozzle | Performing Operations; Transporting | 6 | Active |
| US9840967B2 | Ram air thermal management system | Emerging Cross-Sectional Technologies | 6 | Active |
| US10371093B2 | Aircraft nozzle with a variable nozzle area of a second flow path | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US10718229B2 | Infrared suppression system in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US5323606A | Stowable nozzle | Mechanical Engineering; Lighting; Heating | 4 | Expired |
| US10208668B2 | Turbine engine advanced cooling system | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10767559B2 | Adaptive-area inertial particle separators | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9464594B2 | Compact actuation system for flow nozzle | Emerging Cross-Sectional Technologies | 3 | Active |
| US10378477B2 | Nozzle for jet engines | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9091229B2 | Aircraft powerplant | Emerging Cross-Sectional Technologies | 2 | Active |
| US11513234B2 | Estimating device position in multipath environments | Physics | 1 | Active |
| US11339745B1 | Dual flowpath exhaust for fuel cooling in a hypersonic propulsion system | Emerging Cross-Sectional Technologies | 1 | Active |
| US12065965B1 | Rotating detonation augmentors with adjustable throats for gas turbine engines | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12025074B1 | Plug nozzle for high mach gas turbine engines | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10730636B2 | Integrated aircraft cooling system | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.